BACKGROUND
[0001] Many resonant fiber optic gyroscopes (RFOGs) use free-space optical benches on which
many of the optical components bridge the fiber resonator coil with the laser beam
generators. The many discrete optical components include, but are not limited to,
beam-splitters, ball lenses and half waveplates. These many discreate optical components
on the free-space optical bench can increase the complexity and cost of the RFOG.
However, these negative side effects are often overlooked due to the transfer efficiency
between the fiber resonator coil and the beam generator provided by miniature free-space
optics bench. These free-space optics allow for interfacing between the fiber resonator
coil and the beam generators.
[0002] Recent advancements in integrated photonics provided a means for interfacing with
fiber optics, demonstrating high degrees of robustness, resulting in reduced size,
weight, and power consumption when compared to free-spaced optics. Thus, the integrated
photonics platform offers a high-efficiency coupler with the ability to be applied
to many different integrated photonics platforms.
SUMMARY
[0003] The Embodiments of the present invention provide methods and systems for an RFOG
using at least two integrated photonics interfaces and will be understood by reading
and studying the following specification.
[0004] In an example, a system is provided, the system comprising: at least two integrated
photonics interfaces, each of the at least two integrated photonics interfaces having
a proximal end and a distal end, each of the at least two integrated photonics interfaces
having a waveguide structure including, a first waveguide layer extending from the
proximal end to the distal end of the integrated photonics interface, the first waveguide
layer including a first waveguide branch that extends from the proximal end to the
distal end of the integrated photonics interface and a second waveguide branch that
extends from the proximal end to the distal end of the integrated photonics interface,
and a second waveguide layer separated from the first waveguide layer, the second
waveguide layer extending from the proximal end to the distal end of the integrated
photonics interface, the second waveguide layer including a including a third waveguide
branch that extends from the proximal end to the distal end of the integrated photonics
interface and a fourth waveguide branch that extends from the proximal end to the
distal end of the integrated photonics interface; an optical resonator coil comprising
a first port and a second port, wherein the first port is optically coupled to the
proximal end of a first integrated photonics interface of the at least two integrated
photonics interfaces and the second port is optically coupled to the proximal end
of a second integrated photonics interface of the at least two integrated photonics
interfaces; and wherein the waveguide structure is configured to match an integrated
photonics mode to a fiber mode supported by an optical fiber.
DRAWINGS
[0005] Embodiments of the present invention can be more easily understood and further advantages
and uses thereof more readily apparent, when considered in view of the description
of the preferred embodiments and the following figures in which:
Figure 1 is a block diagram of an exemplary embodiment of a resonant fiber optic gyroscope
configured with an integrated photonics interface.
Figure 2 is a perspective side view of a fiber-to-waveguide optical coupler, according
to one embodiment.
Figure 2A is a perspective side view of a fiber-to-waveguide optical coupler, according
to one embodiment.
Figure 3 is a graphical representation of an integrated photonics interface according
to one embodiment.
Figure 4 illustrates an exemplary method of operating a resonant fiber optic gyroscope
with an integrated photonics interface.
[0006] In accordance with common practice, the various described features are not drawn
to scale but are drawn to emphasize features relevant to the present invention. Reference
characters denote like elements throughout figures and text.
DETAILED DESCRIPTION
[0007] In the following detailed description, reference is made to the accompanying drawings
that form a part hereof, and in which is shown by way of specific illustrative embodiments
in which the invention may be practiced. These embodiments are described in sufficient
detail to enable those skilled in the art to practice the invention, and it is to
be understood that other embodiments may be utilized and that logical, mechanical
and electrical changes may be made without departing from the scope of the present
invention. The following detailed description is, therefore, not to be taken in a
limiting sense.
[0008] Embodiments provide a high-efficiency fiber-to-waveguide coupler implemented in a
resonator fiber-optic gyroscope (RFOG) is described herein. The fiber-to-waveguide
coupler includes a multi-layer waveguide structure that matches an integrated photonics
mode to the mode supported by the standard optical fiber. The on-chip design of a
multi-layer waveguide structure enables ultra-high efficiency fiber-to chip transfer
without many of the coupling methodologies which increase the size, cost, and points
of error within a traditional RFOG.
[0009] The multi-layer photonics interface with on-chip design allows sufficiently high
efficiency pass through rates. For an initial hand-off between the fiber mode to the
waveguide mode, the design is theoretically simulated to be greater than about 99%
and the following adiabatic transition into a single waveguide layer is theoretically
simulated to be greater than about 99.9%.
[0010] The on-chip design of the multi-layer waveguide structure enables ultra-high efficiency
fiber-to-chip transfer without ball lens-based coupling methodology. The on-chip waveguides
direct optical signals, eliminating the need for discrete micro-optic beam splitters
to steer optical signals. Furthermore, the waveguide preserves optical signal polarization,
eliminating the need for discrete micro-optic polarizers, half waveplates, and Faraday
rotators, and the polarization ratio can be improved further by incorporating on-chip
polarizing elements into the device design. Because the chip manufacturing is based
on standard, micro- and nanofabrication processes, the design can be produced quickly
and relatively inexpensively.
[0011] Figure 1 illustrates a block diagram of one example embodiment of an RFOG with an
integrated photonics interface 100. The embodiment of Figure 1 is but one RFOG architecture
in which the present invention can be implemented.
[0012] In the illustrated embodiment, the RFOG with an integrated photonics interface 100
includes an optical resonator coil 102, an integrated photonics interface 104, a coherent
light source system 110, and a processing system 108.
[0013] The optical resonator coil 102 has a first port and a second port. The first port
and the second port of the optical resonator coil 102 are coupled to the integrated
photonics interface 104. The integrated photonics interface 104 includes integrated
waveguides which direct optical signals through the integrated photonics interface
104. One of the integrated waveguides closes the loop of the optical resonator coil
102. Other integrated waveguides provide connections for the first port.
[0014] In one embodiment, the optical resonator coil 102 is comprised of turns or windings
of optical fiber. The first photodetector 106a, the second photodetector 106b, the
third photodetector 106c, the fourth photodetector 106d, the fifth photodetector 106e,
and the coherent light source system 110 are coupled to the integrated photonics interface
104.
[0015] Photodetectors convert incident optical signals into electrical signals. The amplitude
of the electrical signal generated by the photodetector is linearly related to the
intensity of the incident optical signal.
[0016] In one embodiment, the processing system 108 is a state machine. In another embodiment,
the processing system comprises a processor circuitry coupled to memory circuitry.
The processing circuitry may be implemented with at least one of a microprocessor,
a microcontroller, an application specific integrated circuit, and/or a gate array.
The memory circuitry may be implemented by at least one of random access memory, read
only memory, Flash memory, magnetic memory such as a hard drive, and/or optical memory
such as an optical drive and optical disc. The processing circuitry may execute software
and/or firmware stored in the memory circuitry, e.g. to determine angular rate of
rotation.
[0017] The processing system 108 determines the angular rate of rotation of the optical
resonator coil 102 by processing signals from the coherent light source system 110.
The memory may include program instructions which are executed by the processor to
determine the angular rate of rotation 115 of the optical resonator coil 102 about
an input axis 117. The angular rate of rotation 115 is determined by the difference
between the resonant frequencies of the optical resonator in the clockwise and counterclockwise
directions. This is measured by locking the frequencies, fcw and fccw, of the clockwise
(CW) slave optical signal (or first optical signal) 111a and the counter-clockwise
(CCW) slave optical signals 103b (or second optical signal) to the CW and CCW resonances,
respectively, of the optical resonator. Thus, the processing system 108 uses a frequency
difference, Δf, between the frequency, fcw, of the CW slave optical signal and the
frequency, fccw, of the CCW slave optical signal to derive the rotation rate output
of the optical resonator, e.g. the RFOG with an optical processing system with optical
power control. The CW optical power is controlled via photodetector 106d, CW optical
Power Servo System 110i and CW VOA 110j, where photodetectors 106d is connected to
the CW optical power control port of the Multi-layer Photonics Interface 104. Likewise,
The CCW optical power is controlled via photodetector 106e, CCW optical Power Servo
System 110m and CW VOA 110k, where photodetectors 106e is connected to the CCW optical
power control port of the Multi-layer Photonics Interface 104..
[0018] In the illustrated embodiment, the first optical signal 111a is combined with a master
optical signal (or second optical signal) 111b in an optical combiner (combiner) 110i
prior to being coupled to the integrated photonics system 104, and then to the optical
resonator coil 102. The CCW slave optical signal 103b is also coupled to the integrated
photonics system 104 and the optical resonator coil 102. Signals representative of
fccw and fcw are respectively provided by a CCW resonance tracking servo system 110h
and a CW resonance tracking servo system 110g in the coherent light source system
110. The angular rate of rotation 115 about the input axis 117 is an angular rate
of rotation, Ω, 115 where Ω = (λ
∗ Δf
∗ P) / (4
∗ A), λ is substantially equal to the average wavelength of the clockwise optical signal
103a and the counter-clockwise light signal 103b. Further, A is the area enclosed
by the optical resonator coil 102 and P is the perimeter of the optical resonator
path of the optical resonator coil 102 and the multi-layer photonics interface 104,
optically connecting light between two fiber ends of coil 102.
[0019] The coherent light source system 110 generates a clockwise (CW) optical signal 103a
and counter-clockwise (CCW) optical signal 103b which are coupled to the optical resonator
coil 102 by the integrated photonics system 104. In one embodiment, the CW optical
signal 103a and the CCW optical signal 103b are linearly polarized. In another embodiment,
the linearly polarized CW optical signal 103a and the linearly polarized CCW optical
signal 103b are each substantially linearly polarized in one direction, e.g. horizontal
or vertical, or P or S polarized. The direction of polarization is ideally the same
for the linearly polarized CW optical signal 103a and the linearly polarized CCW optical
signal 103b. Polarized CW optical signal 103a' and polarized CCW optical signal 103b'
propagate respectively clockwise and counter-clockwise around the optical resonator
coil 102.
[0020] The integrated photonics system 104 transfers optical feedback signals which are
converted to electrical feedback signals by the first photodetector 106a, the second
photodetector 106b, the third photodetector 106c, the fourth photodetector 106d, and
the fifth photodetector 106e. The first photodetector 106a, the second photodetector
106b, the third photodetector 106c, the fourth photodetector 106d, and the fifth photodetector
106e respectively generate a first feedback signal 105a, a second feedback signal
105b, a third feedback signal 105c, a fourth feedback signal 105d, and a fifth feedback
signal 105e which are coupled to the coherent light source system 110.
[0021] In the illustrated embodiment, the coherent light source system 110 comprises a PDH
servo system 110a, a CW slave optical source 110c, a master optical source 110b, a
CCW slave optical source 110d, a CW resonance tracking servo 110g, a CW optical phase
lock loop 110e, a CCW optical phase lock loop 110f, a CCW resonance tracking servo
system 110h, an optical combiner (combiner) 110i, a CW optical power servo system
1101, a CCW optical power servo system 110m, a CW variable optical attenuator (VOA)
110j, and a CCW VOA 110k. The PDH servo system 110a is configured to receive a first
feedback signal 105a, and is coupled to the master optical source 110b and the first
photodetector 106a.
[0022] The CW resonance tracking servo 110g is configured to receive the third feedback
signal 105c, and is coupled to the CW optical phase lock loop 110e and the third photodetector
106c. The CW optical phase lock loop 110e is coupled to the CW slave optical source
110c and the master optical source 110b. The CCW resonance tracking servo system 110h
is configured to receive the second feedback signal 105b, and is coupled to the CCW
optical phase lock loop 110f and the second photodetector 106b. The CCW optical phase
lock loop 110f is coupled to the CCW slave optical source 110d and the master optical
source 110b.
[0023] The CW optical power servo system 1101 is configured to receive the fourth feedback
signal 105d, and is coupled to the CW VOA 110j and the fourth photodetector 106d.
The CCW optical power servo system 110m is configured to receive the fifth feedback
signal 105e, and is coupled to the CCW VOA 110k. The fourth photodetector 106d and
the fifth photodetector 106e receive respectively a portion of the CW optical signal
103a' and a portion of the CCW optical signal 103b' circulating in the optical resonator,
and convert such optical signals respectively to electrical signals, respectively
the fourth feedback signal 105d and the fifth feedback signal 105e. The amplitude
of the fourth feedback signal 105d and the fifth feedback signal 105e is indicative
of the power levels of respectively the CW optical signal 103a' and the CCW optical
signal 103b'. The fourth feedback signal 105d and the fifth feedback signal 105e are
respectively received by the CW optical power servo system 1101 and the CCW optical
power servo system 110m. The CW optical power servo system 1101 and the CCW optical
power servo system 110m are electrical circuits configured to generate electrical
signals to control the attenuation of respectively the CW VOA 110j and the CCW VOA
110k to maintain a constant power level of the CW optical signal 103a' and the CCW
optical signal 103b' propagating in the optical resonator 102. Although, a variable
optical attenuator is illustrated for pedagogical purposes herein, other devices such
as a variable gain optical amplifier can be used in lieu of a variable optical attenuator.
[0024] The optical combiner 110i combines a first optical signal 111a emitted from the CW
slave optical source 110c and a second optical signal 111b emitted from the master
optical source 110b, and forms the CW optical signal 103a. The CCW slave optical source
110d generates the CCW optical signal 103b.
[0025] The first feedback signal 105a and the PDH servo system 110a lock the carrier frequency
of the second optical signal 111b emitted by the master optical source 110b to a longitudinal
resonant frequency or to a frequency that is offset from a longitudinal resonant frequency
of the optical resonator by a fixed frequency (offset frequency). The longitudinal
resonant frequency equals q multiplied by a free spectral range (FSR) of the optical
resonator, where q is an integer. In some embodiments, the carrier frequency of the
second optical signal 111b is locked to q times FSR, or in some embodiments it is
locked to (q + ½)
∗ FSR. The difference between the longitudinal resonance frequency (or resonance frequency)
and the corresponding carrier frequency is the frequency offset.
[0026] The third feedback signal 105c and the CW resonance tracking servo system 110g and
the CW optical phase lock loop 110e lock the carrier frequency of the first optical
signal 111a emitted by the CW slave optical source 110c to a resonant frequency or
to a frequency that is offset from a CW resonant frequency of the optical resonator
by a fixed offset frequency. The CW resonant frequency equals p multiplied by a free
spectral range (FSR) of the optical resonator, where p is an integer. In some embodiments,
the carrier frequency of the first optical signal 111a is locked to p times FSR, or
in some embodiments it is locked to (p + ½)
∗ FSR.
[0027] The second feedback signal 105b, the CCW resonance tracking servo system 110h, and
CCW optical phase lock loop 110f lock the carrier frequency of the CCW optical signal
103b emitted by the CCW slave optical source 110d to a resonant frequency or to a
frequency that is offset from a CCW resonant frequency of the optical resonator by
a fixed offset frequency. The CCW resonant frequency equals m multiplied by a free
spectral range (FSR) of the optical resonator, where m is an integer. In some embodiments,
the carrier frequency of the CCW optical signal 103b is locked to m times FSR, or
in some embodiments it is locked to (m + ½)
∗ FSR. In one embodiment, q, p, and m are different integer numbers.
[0028] When the CW and CCW carrier frequencies are both locked to offset frequencies, the
frequency offsets from optical resonator resonant frequencies are substantially equal;
hence, the difference between the carrier frequencies of the first optical signal
111a and the CCW optical signal 103b are equal to Δf as described above, and rotation
rate can be derived from Δf as described above.
[0029] In one embodiment, the frequency offsets of the first optical signal 111a and the
CCW optical signal 103b are substantially zero frequency. In another embodiment, each
frequency offset is substantially one half of a free spectral range of the optical
resonator. In all embodiments, the first optical signal 111a, the second optical signal
111b, and CCW optical signal 103b are frequency modulated, e.g. by frequency modulating
respectively the CW slave optical source 110c, the master optical source 110b, and
the CCW slave optical source 110d, to determine optical resonator resonant frequencies.
In one embodiment, modulation frequencies for the CW slave optical source 110c, the
master optical source 110b, and the CCW slave optical source 110d are all different,
so that the CCW resonance tracking servo system 110h, the CW resonance tracking servo
system 110g, and the PDH servo system 110a may distinguish detected optical signals
from each of the CW slave optical source 110c, the master optical source 110b, and
the CCW slave optical source 110d. The frequency modulation causes each of the first
optical signal 111a, the second optical signal 111b, and the CCW optical signal 103b
to have a spectrum of frequencies centered about a corresponding carrier frequency.
[0030] In embodiments where the carrier frequencies of the first optical signal 111a and
the CCW optical signal 103b, respectively emitted by the CW slave optical source 110c
and the CCW slave optical source 110d, are locked to a frequency offset of substantially
one half free spectral range from a resonant frequency of the optical resonator in
the CW and CCW directions respectively, the odd sidebands of the CW slave optical
source 110c and the CCW slave optical source 110d are locked onto resonant frequencies
in the CW and CCW directions respectively. This condition is substantially the same
for measuring rotation rate as the case of locking CW and CCW slave optical source
carrier frequencies to CW and CCW resonant frequencies of the optical resonator.
[0031] In one embodiment, the carrier frequencies of first optical signal 111a, the second
optical signal 111b, and the CCW optical signal 103b are controlled as follows. The
carrier frequency of the second optical signal 111b is locked to a resonance or an
offset frequency corresponding to the CW direction of the optical resonator as shown
in Figure 1. The photodetector PD1 106a detects an incident optical signal, and generates
the corresponding first feedback 105a which is provided to the PDH servo system 110a.
The PDH servo system 110a is responsive to a frequency component in first feedback
signal 105a that is related to the frequency of modulation applied to the carrier
frequency of the master optical source 110b. Portions of the second optical signal
111b, emitted by the master optical source 110b, are respectively coupled to the CW
optical phase lock loop 110e and the CCW optical phase lock loop 110f. A portion of
the first optical signal 111a, emitted by the CW slave optical source 110c, and a
portion of the CCW optical signal 103b, emitted by the CCW slave optical source 110d,
are respectively coupled to the CW optical phase lock loop 110e and the CCW optical
phase lock loop 110f. The carrier frequency of the first optical signal 111a is locked
to the carrier frequency of the second optical signal 111b within a tunable difference
frequency of fl by the CW optical phase lock loop 110e. The carrier frequency of the
CCW optical signal is locked to the master carrier frequency within a tunable difference
frequency of f2 by the CCW optical phase lock loop 110f. A tunable difference frequency
is a frequency within the tuning range of the corresponding servo system. The CW resonance
tracking servo system 110g and the CCW resonance tracking servo system 110h control
tunable difference frequencies f1 and f2 so that the carrier frequency of the first
optical signal 111a is locked to the CW resonance of the optical resonator (or at
a frequency offset of substantially one half free spectral range from it) and the
carrier frequency of the CCW optical signal 103b is locked to the CCW resonance of
the optical resonator (or to a frequency offset of substantially one half free spectral
range from it). The tunable difference frequencies f1 and f2 are controlled such that
the desirable offset of the CW and CCW carrier frequencies from resonance (e.g., substantially
zero or substantially one half free spectral range) are maintained during rotation
rate changes, and changing environmental conditions, e.g. temperature and vibrations,
that can cause the optical resonator resonances to shift over time.
[0032] As shown in Figure 1, the first optical signal 111a emitted from the CW slave optical
source 110c and the second optical signal 111b emitted from the master optical source
110b are combined in optical combiner 110i prior to being coupled to the integrated
photonics system 104. Optical combiner 110i may be a bulk optic beam splitter, or
a fiber optical direction coupler, or another waveguide directional optical coupler.
[0033] In one embodiment, the master optical source 110b, the CW slave optical source 110c
and the CCW slave optical source 110d each respectively comprise a LASER. Each optical
source may include two or more optical outputs provided, e.g., to the optical resonator
and optical phase lock loop(s) and implemented with an optical splitter. One or more
optical sources may include a phase modulator to frequency modulate respective LASER(s).
One or more optical sources may include intensity (or amplitude) modulators to compensate
for phase modulation to amplitude modulation noise in phase modulator(s), to equalize
the amplitude levels of the baseband component emitted by the slave optical sources,
and to stabilize the second optical signal 111b emitted by the master optical source
110b. Each optical source may include optical isolators to prevent leakage of undesired
signal into such sources. In another embodiment, the PDH servo system 110a, the CW
resonance tracking servo system 110g, and the CCW resonance tracking servo system
110h are respectively implemented with electronic circuitry.
[0034] The coherent light source system 110, or components therein, may include components
not shown in Figure 1. Such components may be used to amplitude and phase modulate
optical signals, and to amplify or split optical signals. In one embodiment, such
components include variable optical attenuator(s), intensity modulator(s), phase modulator(s),
optical amplifier(s), optical isolator(s), and optical passive device(s).
[0035] Figure 2 illustrates a detailed view of a fiber-to-waveguide optical coupler 200
further exemplified in application number
16/223,548. In some embodiments, the integrated photonics interface shares similar structural
anatomy to the fiber-to-waveguide optical coupler. The optical coupler 200 comprises
a waveguide structure 202 surrounded by and embedded in a cladding 204. The waveguide
structure 202 includes a first waveguide layer 210, and a second waveguide layer 220
separated from the first waveguide layer 210 by a predetermined distance. In some
embodiments, more than two waveguide layers may be used, with each subsequent waveguide
using either the structure of the first waveguide layer 210 or the structure of the
second waveguide layer 220 as described below.
[0036] The first waveguide layer 210 has a proximal end 212 and a distal end 214. The first
waveguide layer 210 includes a first pair of waveguides 216, 218 that extend from
the proximal end 212 along a first portion of the first waveguide layer 210. The first
pair of waveguides 216, 218 each widen along a second portion of the first waveguide
layer 210 such that the first pair of waveguides 216, 218, merge into a single waveguide
219 toward the distal end 214.
[0037] The second waveguide layer 220 has a proximal end 222 and a distal end 224. The second
waveguide layer 220 includes a second pair of waveguides 226, 228 that extend from
the proximal end 222 along a first portion of the second waveguide layer 220. The
second pair of waveguides 226, 228 each narrow along a second portion of the second
waveguide layer 220 to respective distal tips 227, 229 at the distal end 224.
[0038] The waveguide structure 220 is configured to couple an optical fiber 240 to an integrated
photonics platform, such that an integrated photonics mode is matched to a fiber mode
supported by an optical fiber 240.
[0039] The first and second waveguide layers 210, 220 can be composed of various higher
index optically transmissive materials, such as silicon, silicon nitride (SiNx), silicon
oxynitride (SiON), silicon carbide (SiC), diamond, silicon germanium (SiGe), germanium,
gallium arsenide (GaAs), gallium nitride (GaN), gallium phosphide (GaP), lithium niobite
(LiNbO
3), titanium dioxide (TiO
2), or combinations thereof.
[0040] The cladding 204 can be composed of various lower index materials, such as silicon
dioxide (SiO
2), silicon oxynitride (SiON), zinc oxide (ZnO) (used with Si waveguide or other similarly
high index waveguide), aluminum oxide (Al
2O
3), calcium fluoride (CaF
2), or combinations thereof.
[0041] The first pair of waveguides 216, 218 can each have a thickness of about 25 nm to
about 100 nm, and the second pair of waveguides 226, 228 can each have a thickness
of about 25 nm to about 100 nm.
[0042] Figure 2a illustrates a detailed view of a fiber-to-waveguide optical coupler 200a.
In some embodiments, the integrated photonics interface shares similar structural
anatomy to the fiber-to-waveguide optical coupler. The optical coupler 200a comprises
a waveguide structure 202a surrounded by and embedded in a cladding 204a. The waveguide
structure 202a includes a first waveguide layer 210a, and a second waveguide layer
220a separated from the first waveguide layer 210a by a predetermined distance.
[0043] The first waveguide layer 210a has a proximal end 212a and a distal end 214a. The
first waveguide layer 210a includes a first pair of waveguides 216a, 218a that extend
from the proximal end 212a along a first portion of the first waveguide layer 210a.
In some embodiments, the first pair of waveguides 216a, 218a each narrow along a second
portion of the first waveguide layer 210a to respective distal tips 217a, 219a at
the distal end 214a.
[0044] The second waveguide layer 220a has a proximal end 222a and a distal end 224a. The
second waveguide layer 220a includes a second pair of waveguides 226a, 228a that extend
from the proximal end 222a along a first portion of the second waveguide layer 220a.
In some embodiments, the second pair of waveguides 226a, 228a each narrow along a
second portion of the second waveguide layer 220a to respective distal tips 227a,
229a at the distal end 224a.
[0045] The waveguide structure 220a is configured to couple an optical fiber 240a to an
integrated photonics platform, such that an integrated photonics mode is matched to
a fiber mode supported by an optical fiber 240a.
[0046] In some embodiments, the first pair of waveguides 216a, 218a and the second pair
of waveguides 226a, 228a do not narrow along the second portion of the respective
waveguide layers 210a, 220a. In some embodiments, the first pair of waveguides 216a,
218a comprise a first pair of waveguides for a second fiber-to-waveguide optical coupler.
Similarly, the second pair of waveguides 226a, 228a comprise a second pair of waveguides
for a second optical coupler. At the distal end 214a, the first pair of waveguides
216a couple to a second optical fiber opposite the optical fiber 240a. Similarly,
at the distal end 224a, the second pair of waveguides 226a couple to the second optical
fiber opposite the optical fiber 240a. Thus, the optical fiber 240a and the second
optical fiber optically couple along the first pair of waveguides 216a, 218a and the
second pair of waveguides 226a, 228a. The two fiber-to-waveguide optical couplers
share the first waveguide layer 210a and the second waveguide layer 220a.
[0047] The first and second waveguide layers 210a, 220a can be composed of various higher
index optically transmissive materials, such as silicon, silicon nitride (SiNx), silicon
oxynitride (SiON), silicon carbide (SiC), diamond, silicon germanium (SiGe), germanium,
gallium arsenide (GaAs), gallium nitride (GaN), gallium phosphide (GaP), lithium niobite
(LiNbO
3), titanium dioxide (TiO
2), or combinations thereof.
[0048] The cladding 204a can be composed of various lower index materials, such as silicon
dioxide (SiO
2), silicon oxynitride (SiON), zinc oxide (ZnO) (used with Si waveguide or other similarly
high index waveguide), aluminum oxide (Al
2O
3), calcium fluoride (CaF
2), or combinations thereof.
[0049] The first pair of waveguides 216a, 218a can each have a thickness of about 25 nm
to about 100 nm, and the second pair of waveguides 226a, 228a can each have a thickness
of about 25 nm to about 100 nm.
[0050] Figure 3 is an example graphical representation of an integrated photonics interface
300. In the example, the integrated photonics interface 300 comprises four waveguides:
a first waveguide 302, a second waveguide 312, a third waveguide 322, and a fourth
waveguide 332 integrated into one or more layers of the integrated photonics interface
300. The integrated photonics interface 300 can be a multi-layer photonics interface
where each layer comprises one or more waveguides. The orientation and scale of the
waveguides on the integrated photonics interface are scaled to exemplify the features
of the device, and should not be considered the actual orientation of the waveguides
within the integrated photonics interface 300. In some examples, the waveguides comprise
a high index optically transmissive material.
[0051] In the example, the first waveguide 302 comprises a first port 304 and a second port
306. The waveguides of the integrated photonics interface 300 are configured to preserve
the optical signal polarization and to guide the optical signal with little signal
loss. In the example, the first port 304 and the second port 306 of the first waveguide
302 optically couple to an optical resonator coil, a fiber resonator coil, or another
type of resonator. The optical couplings at the first port 304 and the second port
306 of the first waveguide 302 are configured preserve the signal polarization and
preserve greater than 99% of the signal. In some examples, connections at the first
port 304 and the second port 306 comprise an integrated photonics interface as depicted
in Figure 2.
[0052] In the example, the second waveguide 312 comprises a first port 314 and a second
port 316. In the example, the first port 314 and the second port 316 of the second
waveguide 312 are a first beam transmission port and a second beam transmission port
respectively. In some examples, the first port 314 and the second port 316 of the
second waveguide 312 each optically couple to one or more photodetectors within an
RFOG. In the example given in Figure 1, the first port 314 couples to the second photodetector
106b and the second port 316 couples to the third photodetector 106c. The second waveguide
312 is configured to be optically coupled 318 to the first waveguide 302. The optical
coupling 318 is configured to allow a portion of the light transmitted through the
first waveguide 302 through to the second waveguide 312. In some examples, connections
at the first port 314 and the second port 316 comprise an integrated photonics interface
as depicted in Figure 2.
[0053] In the example, the third waveguide 322 comprises a first port 324 and a second port
326. In the example, the first port 324 and the second port 326 of the third waveguide
322 are a first beam reflection port and a Multi-frequency laser source port respectively
and optically couple to the Multi-frequency laser source. In some examples, the first
port 324 of the third waveguide 322 each optically couples to a photodetector within
an RFOG. The third waveguide 322 is configured to be optically coupled 328 to the
first waveguide 302. The optical coupling 328 is configured to allow a portion of
the light transmitted through the third waveguide 322 through to the first waveguide
302 and thus the attached resonator coil. In some examples, connections at the first
port 324 and the second port 326 comprise an integrated photonics interface as depicted
in Figure 2.
[0054] In the example, the fourth waveguide 332 comprises a first port 334 and a second
port 336. In the example, the first port 334 and the second port 336 of the fourth
waveguide 332 are a Multi-frequency laser source port and a second beam reflection
port respectively and optically couple to the Multi-frequency laser source. In some
examples, the second port 336 of the fourth waveguide 332 each optically couples to
a photodetector within an RFOG. The fourth waveguide 332 is configured to be optically
coupled 338 to the first waveguide 302. The optical coupling 338 is configured to
allow a portion of the light transmitted through the third waveguide 332 through to
the first waveguide 302 and thus the attached resonator coil. In some examples, connections
at the first port 334 and the second port 336 comprise an integrated photonics interface
as depicted in Figure 2.
[0055] The waveguides 302, 312, 322, 332 of the integrated photonics interface 300 can be
composed of various higher index optically transmissive materials, such as silicon,
silicon nitride (SiNx), silicon oxynitride (SiON), silicon carbide (SiC), diamond,
silicon germanium (SiGe), germanium, gallium arsenide (GaAs), gallium nitride (GaN),
gallium phosphide (GaP), lithium niobite (LiNbO
3), titanium dioxide (TiO
2), or combinations thereof.
[0056] The waveguides 302, 312, 322, 332 of the integrated photonics interface 300 can each
have a thickness of about 25 nm to about 100 nm, and the second pair of waveguides
226, 228 can each have a thickness of about 25 nm to about 100 nm.
[0057] Figure 4 illustrates an exemplary method 400 of operating an RFOG with an integrated
photonics interface. To the extent the method 400 shown in Figure 4 is described as
being implemented in the system shown in Figure 1 and Figure 3, it is to be understood
that other embodiments can be implemented in other ways. The blocks of the flow diagram
have been arranged in a generally sequential manner for ease of explanation; however,
it is to be understood that this arrangement is merely exemplary, and it should be
recognized that the processing associated with the methods (and the blocks shown in
the figures) can occur in a different order (for example, where at least some of the
processing associated with the blocks is performed in parallel and/or in an event-driven
manner).
[0058] In block 440, receive at an integrated photonics interface a first optical signal
and a second optical signal, e.g. from the coherent light source system 110. The first
optical signal and the second optical signal are received at separate waveguides within
the integrated photonics interface. In some examples, the waveguides are on the same
layer of the integrated photonics interface, in other examples, the waveguides are
on separate layers.
[0059] In block 442, inject a portion of the first optical signal into a first waveguide
within the integrated photonics interface, the first waveguide optically coupled to
an optical resonator, so that the first optical signal propagates in a first direction
through the optical resonator. In block 444, inject a portion of the second optical
signal into the first waveguide within the integrated photonics interface so that
the second optical signal propagates in a second direction through the optical resonator
which is opposite to the first direction.
[0060] In block 446, emit a portion of the first optical signal propagating in the first
direction in the optical resonator. In block 448, emit a portion of the second optical
signal propagating in the second direction in the optical resonator. In block 450,
couple, by the integrated photonics interface, a portion of the emitted first optical
signal to a first power detector. In block 452, couple, by the integrated photonics
interface, a portion of the emitted second optical signal to a second power detector.
In block 454, detect, with the first power detector, a power level of at least a portion
of the coupled first optical signal. In block 456, detect, with the second power detector,
a power level of at least a portion of the coupled second optical signal. In block
458, adjust the power level of the received first optical signal. In block 460, adjust
the power level of the received second optical signal.
Exemplary Embodiments
[0061] Example 1 includes system comprising: at least two integrated photonics interfaces,
each of the at least two integrated photonics interfaces having a proximal end and
a distal end, each of the at least two integrated photonics interfaces having a waveguide
structure including, a first waveguide layer extending from the proximal end to the
distal end of the integrated photonics interface, the first waveguide layer including
a first waveguide branch that extends from the proximal end to the distal end of the
integrated photonics interface and a second waveguide branch that extends from the
proximal end to the distal end of the integrated photonics interface, and a second
waveguide layer separated from the first waveguide layer, the second waveguide layer
extending from the proximal end to the distal end of the integrated photonics interface,
the second waveguide layer including a including a third waveguide branch that extends
from the proximal end to the distal end of the integrated photonics interface and
a fourth waveguide branch that extends from the proximal end to the distal end of
the integrated photonics interface; an optical resonator coil comprising a first port
and a second port, wherein the first port is optically coupled to the proximal end
of a first integrated photonics interface of the at least two integrated photonics
interfaces and the second port is optically coupled to the proximal end of a second
integrated photonics interface of the at least two integrated photonics interfaces;
and wherein the waveguide structure is configured to match an integrated photonics
mode to a fiber mode supported by an optical fiber.
[0062] Example 2 includes the system of Example 1, wherein the first waveguide branch of
the first waveguide layer and the second waveguide branch of the first waveguide layer
converge at the distal end of the integrated photonics interface.
[0063] Example 3 includes the system of Examples 1-2, wherein the distal end of the first
integrated photonics interface is coupled to the distal end of the second integrated
photonics interface to form a first waveguide.
[0064] Example 4 includes the system of Examples 1-3, wherein the first waveguide layer
and the second waveguide layer of at least one of the at least two integrated photonics
interfaces comprise a high index optically transmissive material.
[0065] Example 5 includes the system of Examples 1-4, wherein the first waveguide layer
and the second waveguide layer of the at least one of the at least two integrated
photonics interfaces comprise silicon, silicon nitride, silicon oxynitride, silicon
carbide, diamond, silicon germanium, germanium, gallium arsenide, gallium nitride,
gallium phosphide, lithium niobite, titanium dioxide, or combinations thereof.
[0066] Example 6 includes the system of Examples 1-5, wherein the distal end of the first
integrated photonics interface is coupled to the distal end of the second photonics
interface.
[0067] Example 7 includes the system of Examples 1-6, wherein the first waveguide layer
and the second waveguide layer of at least one of the at least two integrated photonics
interfaces have a thickness of about 25 nm to about 100 nm.
[0068] Example 8 includes the system of Examples 1-7, wherein the first waveguide layer
and the second waveguide layer of the at least one of the at least two integrated
photonics interfaces are separated by a distance of about 2.5 µm to about 3.5 µm.
[0069] Example 9 includes the system of Example 1-8, wherein the first waveguide layer and
the second waveguide layer of at least one of the at least two integrated photonics
interfaces are embedded in a cladding.
[0070] Example 10 includes the system of Example 9, wherein the cladding comprises a low
index material.
[0071] Example 11 includes the system of Examples 9-10, wherein the cladding comprises silicon
dioxide, silicon oxynitride, zinc oxide, aluminum oxide, calcium fluoride, or combinations
thereof.
[0072] Example 12 includes the system of Example 3-11, further comprising: a second waveguide
including, a third integrated photonics interface, a fourth integrated photonics interface
that is optically coupled between a distal end of the third integrated photonics interface
and a distal end of the fourth integrated photonics interface; wherein the second
waveguide is optically coupled to the first waveguide; a third optical waveguide including,
a fifth integrated photonics interface, a sixth integrated photonics interface that
is optically coupled between a distal end of the fifth integrated photonics interface
and a distal end of the sixth integrated photonics interface; wherein the third waveguide
is optically coupled to the first waveguide; a fourth optical waveguide including,
a seventh integrated photonics interface, an eighth integrated photonics interface
that is optically coupled between a distal end of the seventh integrated photonics
interface and a distal end of the eighth integrated photonics interface; and wherein
the fourth waveguide is optically coupled to the first waveguide.
[0073] Example 13 includes the system of Example 12, wherein the fifth integrated photonics
interface is optically coupled to a multi-frequency laser source; and wherein the
seventh integrated photonics interface is optically coupled to the multi-frequency
laser source.
[0074] Example 14 includes a system comprising: at least two integrated photonics interfaces,
each of the at least two integrated photonics interfaces having a proximal end and
a distal end, each of the at least two integrated photonics interfaces having a waveguide
structure including, at least two waveguide layers, each waveguide layer extending
from the proximal end to the distal end of the integrated photonics interface, the
first waveguide layer including a first waveguide branch that extends from the proximal
end to the distal end of the integrated photonics interface and a second waveguide
branch that extends from the proximal end to the distal end of the integrated photonics
interface; an optical resonator coil comprising a first port and a second port, wherein
the first port is optically coupled to the proximal end of a first integrated photonics
interface of the at least two integrated photonics interfaces and the second port
is optically coupled to the proximal end of a second integrated photonics interface
of the at least two integrated photonics interfaces; and wherein the waveguide structure
is configured to match an integrated photonics mode to a fiber mode supported by an
optical fiber.
[0075] Example 15 includes the system of Example 14, wherein the first waveguide branch
of the first waveguide layer and the second waveguide branch of the first waveguide
layer converge at the distal end of the integrated photonics interface.
[0076] Example 16 includes the system of Examples 14-15, wherein the each of at least two
waveguide layers of the at least two integrated photonics interfaces are separated
from each other layer by a distance of about 2.5 µm to about 3.5 µm.
[0077] Example 17 includes a method, comprising: receiving a first optical signal and a
second optical signal; communicating a portion of the first optical signal into an
optical resonator through a first integrated photonics interface so that the portion
of the first optical signal propagates in a first direction through the optical resonator;
communicating a portion of the second optical signal into the optical resonator through
a second integrated photonics interface so that the portion of the second optical
signal propagates in a second direction through the optical resonator, which is opposite
the first direction; wherein each of the first integrated photonics interface and
the second integrated photonics interface has a proximal end and a distal end, each
of the first integrated photonics interface and the second of the integrated photonics
interface including at least two waveguide layers extending between the proximal end
and a distal end of the integrated photonics interface, the first waveguide layer
including a first waveguide branch that extends from the proximal end to the distal
end of the integrated photonics interface and a second waveguide branch that extends
from the proximal end to the distal end of the integrated photonics interface; emitting
a portion of the first optical signal propagating in the first direction in the optical
resonator; and emitting a portion of the second optical signal propagating in the
second direction in the optical resonator.
[0078] Example 18 includes the method of Example 17, wherein the first waveguide branch
of the first waveguide layer and the second waveguide branch of the first waveguide
layer couple at the distal end.
[0079] Example 19 includes the method of Examples 17-18, wherein the first integrated photonics
interface and the second integrated photonics interface are on a multi-layer photonics
chip.
[0080] Example 20 includes the method of Examples 17-19 wherein the multi-layer photonics
chip comprises on-chip routing architecture.
1. A system comprising:
at least two integrated photonics interfaces (200), each of the at least two integrated
photonics interfaces (200) having a proximal end (212, 222) and a distal end (214,
224), each of the at least two integrated photonics interfaces (200) having a waveguide
structure (202) including,
a first waveguide layer (210) extending from the proximal end (212) to the distal
end (214) of the integrated photonics interface (200), the first waveguide layer (210)
including a first waveguide branch (216) that extends from the proximal end (212)
to the distal end (214) of the integrated photonics interface (200) and a second waveguide
branch (218) that extends from the proximal end (212) to the distal end (214) of the
integrated photonics interface (200), and
a second waveguide layer (220) separated from the first waveguide layer (210), the
second waveguide layer (220) extending from the proximal end (222) to the distal end
(224) of the integrated photonics interface (200), the second waveguide layer (220)
including a including a third waveguide branch (226) that extends from the proximal
end (222) to the distal end (224) of the integrated photonics interface (200) and
a fourth waveguide branch (228) that extends from the proximal end (222) to the distal
end (224) of the integrated photonics interface (200);
an optical resonator coil (102) comprising a first port (304) and a second port (306),
wherein the first port (304) is optically coupled to the proximal end (212, 222) of
a first integrated photonics interface of the at least two integrated photonics interfaces
and the second port (306) is optically coupled to the proximal end (212, 222) of a
second integrated photonics interface of the at least two integrated photonics interfaces
(200); and
wherein the waveguide structure is configured to match an integrated photonics mode
to a fiber mode supported by an optical fiber.
2. The system of claim 1, wherein the first waveguide branch (216) of the first waveguide
layer (210) and the second waveguide branch (218) of the first waveguide layer (210)
converge (219) at the distal end (214) of the at least two integrated photonics interfaces
(200).
3. The system of claim 1, wherein the distal end (214, 224) of the first integrated photonics
interface (304) is coupled to the distal end (214, 224) of the second integrated photonics
(306) interface to form a first waveguide (302).
4. The system of claim 1, wherein the first waveguide layer (210) and the second waveguide
layer (220) of the at least one of at least two integrated photonics interfaces (200)
comprise a high index optically transmissive material.
5. The system of claim 1, wherein the first waveguide layer (210) and the second waveguide
layer (220) of the at least one of the at least two integrated photonics interfaces
(200) comprise silicon, silicon nitride, silicon oxynitride, silicon carbide, diamond,
silicon germanium, germanium, gallium arsenide, gallium nitride, gallium phosphide,
lithium niobite, titanium dioxide, or combinations thereof.
6. The system of claim 1, wherein the distal end (214) of the first integrated photonics
interface is coupled to the distal end (214) of the second photonics interface.
7. The system of claim 3, further comprising:
a second waveguide (312) including,
a third integrated photonics interface (314),
a fourth integrated photonics interface (316) that is optically coupled between a
distal end of the third integrated photonics interface (314) and a distal end of the
fourth integrated photonics interface (316);
wherein the second waveguide (312) is optically coupled (318) to the first waveguide
(302);
a third optical waveguide (322) including,
a fifth integrated photonics interface (324),
a sixth integrated photonics (326) interface that is optically coupled between a distal
end of the fifth integrated photonics (324) interface and a distal end of the sixth
integrated photonics interface (326);
wherein the third waveguide (322) is optically coupled (328) to the first waveguide
(302);
a fourth optical waveguide including (332),
a seventh integrated photonics interface (334),
an eighth integrated photonics interface (336) that is optically coupled between a
distal end of the seventh integrated photonics interface (334) and a distal end of
the eighth integrated photonics interface (336); and
wherein the fourth waveguide (332) is optically (338 coupled to the first waveguide
(302).
8. The system of claim 7, wherein the fifth integrated photonics (324) interface is optically
couple to a multi-frequency laser source (103a); and
wherein the seventh integrated photonics interface (334) is optically coupled to the
multi-frequency laser source (103b).
9. A method, comprising:
receiving a first optical signal and a second optical signal (440);
communicating a portion of the first optical signal into an optical resonator through
a first integrated photonics interface so that the portion of the first optical signal
propagates in a first direction through the optical resonator (442);
communicating a portion of the second optical signal into the optical resonator through
a second integrated photonics interface so that the portion of the second optical
signal propagates in a second direction through the optical resonator, which is opposite
the first direction (444);
wherein each of the first integrated photonics interface and the second integrated
photonics interface has a proximal end and a distal end, each first and second photonics
interface including at least two waveguide layers extending between the proximal end
and a distal end of the associated first and second photonics interface, the first
waveguide layer including a first waveguide branch that extends from the proximal
end to the distal end of the associated first and second integrated photonics interface
and a second waveguide branch that extends from the proximal end to the distal end
of the associated first and second integrated photonics interface;
emitting a portion of the first optical signal propagating in the first direction
in the optical resonator (446); and
emitting a portion of the second optical signal propagating in the second direction
in the optical resonator (448).
10. The method of claim 9, wherein the first waveguide branch of the first waveguide layer
and the second waveguide branch of the first waveguide layer couple at the distal
end.